WO2012170188A2 - Exhaust-gas turbocharger - Google Patents
Exhaust-gas turbocharger Download PDFInfo
- Publication number
- WO2012170188A2 WO2012170188A2 PCT/US2012/038784 US2012038784W WO2012170188A2 WO 2012170188 A2 WO2012170188 A2 WO 2012170188A2 US 2012038784 W US2012038784 W US 2012038784W WO 2012170188 A2 WO2012170188 A2 WO 2012170188A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- housing
- turbine
- side flange
- exhaust
- gas turbocharger
- Prior art date
Links
- 239000000463 material Substances 0.000 claims abstract description 22
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims description 2
- 239000002131 composite material Substances 0.000 claims description 2
- 238000004026 adhesive bonding Methods 0.000 claims 1
- 238000005476 soldering Methods 0.000 claims 1
- 238000003466 welding Methods 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 description 4
- 238000005755 formation reaction Methods 0.000 description 4
- 238000011068 loading method Methods 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 2
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910001562 pearlite Inorganic materials 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/403—Casings; Connections of working fluid especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/16—Selection of particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/171—Steel alloys
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
Definitions
- the invention relates to an exhaust-gas turbocharger as per the preamble of claim
- An exhaust-gas turbocharger of said type has not only a compressor with a compressor housing, but also a turbine with a turbine housing which is fastened to a bearing housing via a bearing-housing-side flange.
- an already known generic exhaust-gas turbocharger has a bearing housing produced from a material as a cast part.
- Said cast material may be composed of a pearlitic micro structure which, when heated to over 450°C, begins to lose its structure because the pearlite breaks down into its constituent parts.
- a change in volume of the material takes place and, secondly, the bearing housing loses its hardness (HB).
- Said loss of hardness may be so drastic that, specifically in conjunction with dendritic formation of the matrix of the material, significant crack formations may occur.
- the bearing housing material is subjected to a very high temperature in particular at the contact surface or the fit with respect to the turbine housing, and is additionally subjected to mechanical loading by the clamping forces of the connecting elements.
- said crack formation occurs in the bearing- housing-side flange, which results in a direct leakage of exhaust gas at the connecting point between the bearing housing and the turbine housing.
- the highly loaded contact region between the turbine housing and bearing housing is formed by a material which can be subjected to greater loading.
- the turbine-side bearing housing flange may be replaced by a separate flange composed of a higher-grade material in relation to the known solution.
- the material for the fiange to be mounted separately on the bearing housing is matched in terms of its properties to those of the turbine housing.
- the turbine-housing-side flange may be produced from a high-temperature-resistant ferritic material (for example X22XCrMoV 12-1 (1.4923)) or from an austenitic cast steel (for example GX40MeCrSiNb38-18 (1.4849)).
- a high-temperature-resistant ferritic material for example X22XCrMoV 12-1 (1.4923)
- an austenitic cast steel for example GX40MeCrSiNb38-18 (1.4849)
- connection of the separate turbine-housing-side flange to the bearing housing may be realized by means of screw connections, shrink-fit connections, welded connections, adhesive connections, soldered connections, composite casting or a combination of the above connection types.
- the machining of the bearing housing can preferably be carried out in the conventional way after the fixing of the separate flange to the bearing housing.
- figure 1 shows a sectional perspective illustration of an exhaust-gas turbocharger according to the invention
- figure 2 shows a plan view of the bearing housing of the exhaust-gas turbocharger as viewed from the turbine
- figure 3 shows a section through the bearing housing along the line A-A in figure
- figure 4 shows a perspective illustration of a further embodiment of the bearing housing according to the invention
- figure 5 shows a sectional illustration, corresponding to figure 3, of the bearing housing as per figure 4,
- figure 6 shows a partial view of the bearing housing as per figure 4,
- figure 7 shows an illustration, corresponding to figure 4, of a further embodiment of the bearing housing according to the invention
- figure 8 shows an illustration, corresponding to figure 5, of the bearing housing as per figure 7,
- figure 9 shows an illustration, corresponding to figure 6, of the bearing housing as per figure 7,
- figure 10 shows an illustration, corresponding to figure 7, of a further embodiment of the bearing housing according to the invention.
- figure 11 shows an illustration, corresponding to figure 8, of the bearing housing as per figure 10.
- Figure 1 illustrates an exhaust-gas turbocharger 1 according to the invention which has a compressor 7 and a compressor housing 2.
- the exhaust-gas turbocharger 1 also has a turbine 8 with a turbine housing 3 and has a bearing housing 4 which is connected via a compressor-side flange 5 to the compressor 7 and via a turbine-housing-side flange 6 to the turbine 8 or the turbine housing 3.
- Figures 2 and 3 illustrate a first embodiment of the bearing housing 6 according to the invention of the exhaust-gas turbocharger 1.
- the view in figure 2 is a view from the direction of the turbine 8, and shows the bearing housing 4 with its turbine-housing-side flange 6, wherein, owing to the selected illustration, it is possible to see an arrangement 9 composed of a bush, a lever and a pin, and also two dowel pins 10 and 11.
- Figure 3 shows that the turbine-housing-side flange 6, which is formed as a separate component, is formed as a steel flange which can be either screwed or welded to the bearing housing 4.
- the reference numeral 14 symbolically indicates one of the possible weld points of a multiplicity of weld points.
- FIGS. 4 to 6 illustrate a further embodiment of the bearing housing 4 according to the invention, wherein all of the features which correspond to figures 2 and 3 are denoted by the same reference numerals.
- the flange 6 is cast integrally with the bearing housing 4, wherein figure 5 shows that the connection is realized by means of a suitable shaping 17.
- Figures 4 and 6 furthermore show two recesses 15 and 16 which, in said embodiment, are situated entirely within the surface of the flange 6.
- Figures 7 to 9 illustrate a further design variant of an integrally cast flange 6, wherein figure 8 again shows the form fit 17. Said embodiment otherwise corresponds to the embodiment as per figures 4 to 6, aside from the fact that figure 9 shows that the recesses 15 and 16 are situated partially in the material of the flange 6 and partially in the material of the bearing housing 4.
- Figures 10 and 11 show a variant which substantially corresponds to the embodiment as per figures 2 and 3 and in which the flange 6 is screwed to the bearing housing 4 by means of an internal/external thread 13.
- the recesses 15 and 16 as per figure 9 serve, together with the pressed-in bush 9 or the pressed-in pin 11 (shown in figure 2), as a rotation prevention means.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Supercharger (AREA)
Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014514478A JP6116551B2 (en) | 2011-06-06 | 2012-05-21 | Exhaust gas turbocharger |
CN201280022879.9A CN103534459B (en) | 2011-06-06 | 2012-05-21 | Exhaust turbine supercharger |
DE112012001818.4T DE112012001818T5 (en) | 2011-06-06 | 2012-05-21 | turbocharger |
US14/119,225 US10309415B2 (en) | 2011-06-06 | 2012-05-21 | Exhaust-gas turbocharger |
KR1020137034178A KR101889381B1 (en) | 2011-06-06 | 2012-05-21 | Exhaust-gas turbocharger |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011103420.3 | 2011-06-06 | ||
DE102011103420 | 2011-06-06 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2012170188A2 true WO2012170188A2 (en) | 2012-12-13 |
WO2012170188A3 WO2012170188A3 (en) | 2013-01-31 |
Family
ID=47296677
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2012/038784 WO2012170188A2 (en) | 2011-06-06 | 2012-05-21 | Exhaust-gas turbocharger |
Country Status (6)
Country | Link |
---|---|
US (1) | US10309415B2 (en) |
JP (1) | JP6116551B2 (en) |
KR (1) | KR101889381B1 (en) |
CN (1) | CN103534459B (en) |
DE (1) | DE112012001818T5 (en) |
WO (1) | WO2012170188A2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015117670A (en) * | 2013-12-19 | 2015-06-25 | 大豊工業株式会社 | Turbocharger bearing housing |
EP3228838A1 (en) * | 2016-03-22 | 2017-10-11 | MTU Aero Engines GmbH | Method for the production of a turbomachine casing and casing of a turbomachine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9657596B2 (en) | 2014-09-26 | 2017-05-23 | Electro-Motive Diesel, Inc. | Turbine housing assembly for a turbocharger |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0207697B1 (en) * | 1985-06-26 | 1989-09-06 | AlliedSignal Inc. | Cast stainless steel alloy and method for its manufacture |
US20050011192A1 (en) * | 2001-05-10 | 2005-01-20 | Shinjiroh Ohishi | Surface-reformed exhaust gas guide assembly of vgs type turbo charger, and method surface-reforming component member thereof |
EP1541826A1 (en) * | 2003-12-13 | 2005-06-15 | Ford Global Technologies, LLC | Turbocharger |
US20100054934A1 (en) * | 2007-04-16 | 2010-03-04 | Continental Automotive Gmbh | Exhaust gas turbocharger |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63128243U (en) * | 1987-02-16 | 1988-08-22 | ||
JPH05179406A (en) | 1991-04-15 | 1993-07-20 | Hitachi Metals Ltd | Heat resistant cast steel and its production and parts for internal combustion engine |
JPH0749036A (en) * | 1993-08-05 | 1995-02-21 | Aisan Ind Co Ltd | Turbocharger |
JPH07150962A (en) * | 1993-11-26 | 1995-06-13 | Aisin Seiki Co Ltd | Bearing housing of turbocharger |
US7074009B2 (en) * | 2000-06-07 | 2006-07-11 | Borgwarner, Inc. | Casing assembly for the turbine of an exhaust turbochanger |
CN201041073Y (en) * | 2007-03-19 | 2008-03-26 | 刘忠保 | Electronic control injection gasoline engine air inlet system |
CN201050387Y (en) * | 2007-06-18 | 2008-04-23 | 寿光市康跃增压器有限公司 | Exhaust-driven turbo-charger central rotor device |
JP2010261365A (en) * | 2009-05-07 | 2010-11-18 | Otics Corp | Bearing housing for supercharger |
DE102009025054B4 (en) * | 2009-06-10 | 2015-12-03 | Benteler Automobiltechnik Gmbh | turbine housing |
DE102009042260B4 (en) * | 2009-09-22 | 2015-12-10 | Benteler Automobiltechnik Gmbh | turbocharger |
US10066503B2 (en) * | 2011-12-09 | 2018-09-04 | Borgwarner Inc. | Bearing housing of an exhaust-gas turbocharger |
-
2012
- 2012-05-21 US US14/119,225 patent/US10309415B2/en active Active
- 2012-05-21 KR KR1020137034178A patent/KR101889381B1/en active IP Right Grant
- 2012-05-21 WO PCT/US2012/038784 patent/WO2012170188A2/en active Application Filing
- 2012-05-21 JP JP2014514478A patent/JP6116551B2/en not_active Expired - Fee Related
- 2012-05-21 DE DE112012001818.4T patent/DE112012001818T5/en active Pending
- 2012-05-21 CN CN201280022879.9A patent/CN103534459B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0207697B1 (en) * | 1985-06-26 | 1989-09-06 | AlliedSignal Inc. | Cast stainless steel alloy and method for its manufacture |
US20050011192A1 (en) * | 2001-05-10 | 2005-01-20 | Shinjiroh Ohishi | Surface-reformed exhaust gas guide assembly of vgs type turbo charger, and method surface-reforming component member thereof |
EP1541826A1 (en) * | 2003-12-13 | 2005-06-15 | Ford Global Technologies, LLC | Turbocharger |
US20100054934A1 (en) * | 2007-04-16 | 2010-03-04 | Continental Automotive Gmbh | Exhaust gas turbocharger |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015117670A (en) * | 2013-12-19 | 2015-06-25 | 大豊工業株式会社 | Turbocharger bearing housing |
EP3228838A1 (en) * | 2016-03-22 | 2017-10-11 | MTU Aero Engines GmbH | Method for the production of a turbomachine casing and casing of a turbomachine |
US10634008B2 (en) | 2016-03-22 | 2020-04-28 | MTU Aero Engines AG | Method for manufacturing a housing of a turbomachine and turbomachine housing |
Also Published As
Publication number | Publication date |
---|---|
JP6116551B2 (en) | 2017-04-19 |
DE112012001818T5 (en) | 2014-02-06 |
KR20140038471A (en) | 2014-03-28 |
KR101889381B1 (en) | 2018-08-20 |
JP2014516139A (en) | 2014-07-07 |
CN103534459B (en) | 2017-03-29 |
US10309415B2 (en) | 2019-06-04 |
US20140099196A1 (en) | 2014-04-10 |
WO2012170188A3 (en) | 2013-01-31 |
CN103534459A (en) | 2014-01-22 |
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